Numerical Simulation of High Lift Trapezoidal Wing with Transition Modeling in STAR-CCM+

Description:

Prashanth Shankara, CD-adapco

This article details results from the numerical simulations on the NASA Trapezoidal Wing geometry, focusing on the high lift prediction using the CD-adapco solver STAR-CCM+. Computations and validation were based on the guidelines and experimental data provided for the 1st AIAA High Lift Prediction Workshop (HiLiftPW-1) to assess the numerical prediction capability of STAR-CCM+ for high lift configurations.